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Reusable Cryogenic Tank VHM Using Fiber Optic Distributed Sensing TechnologyThe reusable oxygen and hydrogen tanks are key systems for both the X-33 (sub-scale, sub-orbital technology demonstrator) and the commercial Reusable Launch Vehicle (RLV). The backbone of the X-33 Reusable Cryogenic Tank Vehicle Health Management (VHM) system lies in the optical network of distributed strain temperature and hydrogen sensors. This network of fiber sensors will create a global strain and temperature map for monitoring the health of the tank structure, cryogenic insulation, and Thermal Protection System. Lockheed Martin (Sanders and LMMSS) and NASA Langley have developed this sensor technology for the X-33 and have addressed several technical issues such as fiber bonding and laser performance in this harsh environment.
Document ID
19980069722
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Bodan-Sanders, Patricia
(Lockheed Sanders, Inc. Nashua, NH United States)
Bouvier, Carl
(Lockheed Sanders, Inc. Nashua, NH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 98-1929
NASA/CR-1998-208132
NAS 1.26:208132
Report Number: AIAA Paper 98-1929
Report Number: NASA/CR-1998-208132
Report Number: NAS 1.26:208132
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference and Adaptive Structures Forum
Location: Long Beach, CA
Country: United States
Start Date: April 20, 1998
End Date: April 23, 1998
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Helicopter Society, Inc., American Society of Mechanical Engineers, Alpha STAR Corp.
Funding Number(s)
CONTRACT_GRANT: NCC8-115
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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